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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Axial flow type
Radial flow type
None of the listed here
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

First decreases and then increases
Increases
Remain constant
Decreases

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In two cylinders
In two cylinders on both sides of the piston
In one cylinder
In a single cylinder on both sides of the piston

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Volumetric efficiency
Adiabatic efficiency
Isothermal efficiency
Mechanical efficiency

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Higher at high speed
Lower at low speed
Same at all altitudes
Higher at high altitudes

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Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Fatigue
Creep
Toughness
Corrosion resistance

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